Description Winner of the Summerfield Book Award. Design and R&D engineers and students will value the comprehensive, meticulous coverage in this volume, which, under the expert editorial supervision of Gordon C. Oates, features the invited work of prominent specialists in aircraft gas turbine engines. Beginning with the basic principles and concepts of aeropropulsion combustion, chapters explore specific processes, limitations, and analytical methods as they bear on component design.


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    Title :

    Computation of Turbomachinery Boundary Layers


    Contributors:


    Publication date :

    1985-01-01




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





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